Air enters a frictionless, constant area duct with Ma = 2.5,T0 = 20 C, and p0 = 101
Chapter 11, Problem 11.69(choose chapter or problem)
Air enters a frictionless, constant area duct with Ma = 2.5,T0 = 20 C, and p0 = 101 kPa(abs). The gas is decelerated byheating until a normal shock occurs where the local Mach numberis 1.3. Downstream of the shock, the subsonic flow is acceleratedwith heating until it exits with a Mach number of 0.9. Determinethe static temperature and pressure, the stagnation temperature andpressure, and the fluid velocity at the duct entrance, just upstreamand downstream of the normal shock, and at the duct exit. Sketchthe temperatureentropy diagram for this flow.
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